圆形穿孔翅片阵列强制对流换热的增强

K. Dhanawade, H. S. Dhanawade
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引用次数: 25

摘要

快速地从受热表面排出热量,降低材料重量和成本,成为内燃机冷却等热交换设备设计的主要任务。超级热交换器的发展需要制造高效的技术,在扩展表面和周围流体之间交换大量的热量。本文报道了在水平矩形风管中,在水平平面上布置圆形穿孔矩形翅片阵列增强换热的实验研究。性能分析中使用的数据是在不同的流量、不同的热输入和几何条件下实验获得的。基于流量平均进口速度和水力直径,实验涵盖了3000-6000的雷诺数范围。间隙比(C/H) 0.45,翅片间距比(S/H) 0.22,风道宽度150mm,高度100mm,实心和穿孔(减重)翅片尺寸均为100mm × 55mm × 3mm。在不同的热输入和流速下,得到了雷诺数和努塞尔数。将多孔翅片阵列的计算结果与其外部尺寸等效的固体翅片阵列进行了比较。结果表明,多孔翅片阵列的换热效果优于固体翅片阵列。
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Enhancement of forced convection heat transfer from fin arrays with circular perforation
Rapid heat removal from heated surfaces and reducing material weight and cost become a major task for design of heat exchanger equipments like Cooling of I C engines. Development of super heat exchangers requires fabrication of efficient techniques to exchange great amount of heat between surface such as extended surface and ambient fluid. The present paper reports, an experimental study to investigate the heat transfer enhancement in rectangular fin arrays with circular perforation equipped on horizontal flat surface in horizontal rectangular duct. The data used in performance analyses were obtained experimentally by varying flow, different heat inputs and geometrical conditions. The experiment covered Reynolds number range from 3000–6000, based on the flow average inlet velocity and hydraulic diameter. Clearance ratio (C/H) 0.45, inter-fin spacing ratio (S/H) 0.22, duct width 150mm, height 100mm and fin size of both solid and perforated (weight reduction) were 100mm × 55mm × 3mm. For various heat inputs and flow rates values of Reynolds and Nusselt number were obtained. The results of perforated fin arrays have been compared with its external dimensionally equivalent solid fin arrays. It shows that enhancement in heat transfer of perforated fin arrays than solid fin arrays.
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